FIELD: gas turbine engines.
SUBSTANCE: invention relates to a unit for a gas turbine engine with a longitudinal axis, containing the first annular wall (24), while panels (38) are located radially opposite the said first annular wall (24) around the longitudinal axis (A), forming a surface for the passage of air flow, and each panel (38) is connected to the first annular wall (24) by means of at least one fastening means (72) passing through the opening of the panel (38) and connected to the first annular wall (24) by means of a bushing and an insert forming a spacer.
EFFECT: proposed installation allows to make panels without bosses, which are replaced by inserts that are structurally independent of the panels.
11 cl, 8 dwg
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